SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT

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United States of America Patent

SERIAL NO

15457457

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A method for controlling a pressure control mechanism in a turbofan engine having a precooler permitting heat exchange between ambient air and bleed air includes detecting at least one of an engine failure or a bleed system failure, detecting at least one of an ice condition or an activation of an anti-ice system, and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS CANADA LIMITED PARTNERSHIPMIRABEL QC J7N 3C6

International Classification(s)

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  • 2017 Application Filing Year
  • F02K Class
  • 489 Applications Filed
  • 321 Patents Issued To-Date
  • 65.65 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances201720182019202020212022202320240255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
AFRIANTO, Sigit Pierrefonds, CA 4 73
BROUSSEAU, Jean Pierrefonds, CA 4 73
DESILETS, Valerie Vaudreuil, CA 3 63
HAMEL, Remi Laval, CA 5 65

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Patent Citation Ranking

  • 8 Citation Count
  • F02K Class
  • 21.78 % this patent is cited more than
  • 8 Age
Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges2266714101 - 1011 - 2021 - 3031 - 4041 - 500510152025303540455055606570

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